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Computational Studies for Sonic Boom PredictionOutline: Introduction; Launch Ascent and Vehicle Aerodynamics (LAVA) Framework; 1st AIAA Sonic Boom Prediction Workshop Oblique Shock/Plume Interaction; Summary.
Document ID
20190001988
Acquisition Source
Ames Research Center
Document Type
Presentation
Authors
Housman, Jeffrey (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
March 29, 2019
Publication Date
October 28, 2014
Subject Category
Aerodynamics
Report/Patent Number
ARC-E-DAA-TN18916
Report Number: ARC-E-DAA-TN18916
Meeting Information
Meeting: Applied Modeling and Simulation Seminar Series
Location: Moffett Field, CA
Country: United States
Start Date: October 30, 2014
Sponsors: NASA Ames Research Center
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Sonic Boom
Computational
Prediction

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